UA98686C2 - Deformable rear disc for missile container, including a downstream bearing frame - Google Patents
Deformable rear disc for missile container, including a downstream bearing frameInfo
- Publication number
- UA98686C2 UA98686C2 UAA201008714A UAA201008714A UA98686C2 UA 98686 C2 UA98686 C2 UA 98686C2 UA A201008714 A UAA201008714 A UA A201008714A UA A201008714 A UAA201008714 A UA A201008714A UA 98686 C2 UA98686 C2 UA 98686C2
- Authority
- UA
- Ukraine
- Prior art keywords
- bearing frame
- downstream
- downstream bearing
- rear disc
- disc
- Prior art date
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41F—APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
- F41F3/00—Rocket or torpedo launchers
- F41F3/04—Rocket or torpedo launchers for rockets
- F41F3/042—Rocket or torpedo launchers for rockets the launching apparatus being used also as a transport container for the rocket
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41F—APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
- F41F3/00—Rocket or torpedo launchers
- F41F3/04—Rocket or torpedo launchers for rockets
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41F—APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
- F41F3/00—Rocket or torpedo launchers
- F41F3/04—Rocket or torpedo launchers for rockets
- F41F3/0413—Means for exhaust gas disposal, e.g. exhaust deflectors, gas evacuation systems
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Carbon And Carbon Compounds (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Radar Systems Or Details Thereof (AREA)
- Support Of The Bearing (AREA)
- Closures For Containers (AREA)
- Filling Or Discharging Of Gas Storage Vessels (AREA)
Abstract
The invention relates to an improved deformable downstream disc (56; 156; 256) to be fitted on the bottom of a container (15) for a missile (16) and including a stack of elastic blades (63) clamped between at least an upstream and a downstream thermal protection membrane and sealing membrane (70, 71, 72, 73), and maintained between an upstream bearing frame (61) and a downstream bearing frame (64), characterized in that the downstream bearing frame includes an inner edge (80) having an extension so as to provide the disc with an abutment means defining a position of maximum deformation of the elastic blades.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0850162A FR2926360B1 (en) | 2008-01-11 | 2008-01-11 | DEFORMABLE REAR OPERATOR FOR MISSILE CONTAINER, COMPRISING A FRONT SUPPORT FRAME |
Publications (1)
Publication Number | Publication Date |
---|---|
UA98686C2 true UA98686C2 (en) | 2012-06-11 |
Family
ID=39745427
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
UAA201008714A UA98686C2 (en) | 2008-01-11 | 2009-01-08 | Deformable rear disc for missile container, including a downstream bearing frame |
Country Status (11)
Country | Link |
---|---|
US (1) | US8418593B2 (en) |
EP (1) | EP2229573B1 (en) |
KR (1) | KR101567998B1 (en) |
CN (1) | CN101918786B (en) |
ES (1) | ES2617208T3 (en) |
FR (1) | FR2926360B1 (en) |
MA (1) | MA32051B1 (en) |
PL (1) | PL2229573T3 (en) |
UA (1) | UA98686C2 (en) |
WO (1) | WO2009092938A2 (en) |
ZA (1) | ZA201004820B (en) |
Families Citing this family (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US8300757B2 (en) | 2008-08-08 | 2012-10-30 | Motorola Mobility Llc | Methods for detection of failure and recovery in a radio link |
US8584569B1 (en) * | 2011-12-06 | 2013-11-19 | The United States Of America As Represented By The Secretary Of The Navy | Plume exhaust management for VLS |
FR3039889B1 (en) | 2015-08-05 | 2017-07-28 | Mbda France | FLEXIBLE OPENER FOR MISSILE CONTAINER |
BE1023108B1 (en) | 2015-08-24 | 2016-11-23 | Handi-Move N.V. | Improved clamp and aids for lifting patients using the clamp |
FR3053455B1 (en) * | 2016-07-01 | 2019-04-19 | Mbda France | FLEXIBLE OPENER FOR MISSILE CONTAINER |
CN112985174B (en) * | 2021-02-10 | 2023-01-10 | 上海材料研究所 | Cylindrical orthogonal type sealing rear end cover with rectification effect on shock wave reflection |
Family Cites Families (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4324167A (en) * | 1980-04-14 | 1982-04-13 | General Dynamics, Pomona Division | Flexible area launch tube rear cover |
US4498368A (en) * | 1983-10-06 | 1985-02-12 | The United States Of America As Representedby The Secretary Of The Navy | Frangible fly through diaphragm for missile launch canister |
US4683798A (en) * | 1985-12-27 | 1987-08-04 | General Dynamics, Pomona Division | Gas management transition device |
US4686884A (en) * | 1985-12-27 | 1987-08-18 | General Dynamics, Pomona Division | Gas management deflector |
FR2620808B1 (en) | 1987-09-17 | 1990-01-12 | France Etat Armement | REAR LID FOR MISSILE CONTAINER |
US5194688A (en) * | 1992-01-31 | 1993-03-16 | Hughes Missile Systems Company | Apparatus for limiting recirculation of rocket exhaust gases during missile launch |
JP2001124494A (en) * | 1999-10-25 | 2001-05-11 | Mitsubishi Electric Corp | Discharger for flier |
JP4338004B2 (en) * | 2000-03-16 | 2009-09-30 | 株式会社Ihiエアロスペース | Rocket motor nozzle cover |
JP3448648B2 (en) * | 2000-11-27 | 2003-09-22 | 防衛庁技術研究本部長 | Flying object launcher device |
JP2004077038A (en) * | 2002-08-20 | 2004-03-11 | Mitsubishi Heavy Ind Ltd | Back lid of canister for missile |
US7984675B2 (en) * | 2006-02-21 | 2011-07-26 | Metal Storm Limited | Propellant sealing system for stackable projectiles |
-
2008
- 2008-01-11 FR FR0850162A patent/FR2926360B1/en not_active Expired - Fee Related
-
2009
- 2009-01-08 KR KR1020107015280A patent/KR101567998B1/en active IP Right Grant
- 2009-01-08 PL PL09704545T patent/PL2229573T3/en unknown
- 2009-01-08 US US12/735,379 patent/US8418593B2/en active Active
- 2009-01-08 WO PCT/FR2009/050020 patent/WO2009092938A2/en active Application Filing
- 2009-01-08 CN CN2009801019981A patent/CN101918786B/en not_active Expired - Fee Related
- 2009-01-08 UA UAA201008714A patent/UA98686C2/en unknown
- 2009-01-08 ES ES09704545.4T patent/ES2617208T3/en active Active
- 2009-01-08 EP EP09704545.4A patent/EP2229573B1/en active Active
-
2010
- 2010-07-08 MA MA33001A patent/MA32051B1/en unknown
- 2010-07-08 ZA ZA2010/04820A patent/ZA201004820B/en unknown
Also Published As
Publication number | Publication date |
---|---|
FR2926360A1 (en) | 2009-07-17 |
US8418593B2 (en) | 2013-04-16 |
US20110011251A1 (en) | 2011-01-20 |
ES2617208T3 (en) | 2017-06-15 |
EP2229573B1 (en) | 2016-12-07 |
FR2926360B1 (en) | 2012-10-19 |
KR101567998B1 (en) | 2015-11-10 |
ZA201004820B (en) | 2011-03-30 |
WO2009092938A3 (en) | 2009-12-17 |
WO2009092938A2 (en) | 2009-07-30 |
EP2229573A2 (en) | 2010-09-22 |
MA32051B1 (en) | 2011-02-01 |
CN101918786A (en) | 2010-12-15 |
KR20100122899A (en) | 2010-11-23 |
PL2229573T3 (en) | 2017-05-31 |
CN101918786B (en) | 2013-04-24 |
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